| Registration number |
1969-043A / 03941 |
| Time and date of launch (UT) |
16h.49m.00s. May 18, 1969 |
| Launch site |
Cape Canaveral, LC 39-B |
| Launch vehicle |
Saturn-5 |
| Spacecraft mass (kg) |
48620 |
| Orbital parameters: |
| - inclination (degrees) |
32.5 |
| - period (minutes) |
88.2 |
| - perigee (km) |
185 |
| - apogee (km) |
186 |
| Time and date of landing (UT) |
16h.52m.23s. May 26, 1969 |
| Place of landing |
15.07 S; 164.65 W, miss distance 2.4 km (Pacific Ocean) |
| Duration |
8d.00h.03m.23s. |
| Distance (km) |
1.34 million |
| Number of revolutions around Earth |
1.5 |
| Summary |
Testing of LM in lunar orbit. Spacecraft was at selenocentric orbit for 61h.35m. Undockind, autonomous (stand-alone) fly and docking of LM with CSM. First colour TV translation from space.
|
| Date |
Time (UT) |
Spaceship's revo- lution number |
Explanation |
|
May 18, 1969
|
16:49:00
|
|
Lift-off spacecraft
"Apollo-10"
(crew:
Stafford,
Young,
Cernan
).
|
|
May 18, 1969
|
19:22:27
|
|
S-IVB second burn ignition (for translunar orbit)
|
|
May 18, 1969
|
19:28:10
|
|
Engine cutoff
|
|
May 18, 1969
|
19:51:45
|
|
CSM separated from LM/S-IVB
|
|
May 18, 1969
|
20:06:36
|
|
CSM docked with LM/S-IVB
|
|
May 18, 1969
|
20:45:35
|
|
Separation of CSM from Saturn-IVB
|
|
May 21, 1969
|
06:39:50
|
|
Equigravisphere
|
|
May 21, 1969
|
20:44:54
|
|
Lunar orbit insertion ignition
|
|
May 21, 1969
|
20:50:50
|
|
Engine cutoff
|
|
May 22, 1969
|
19:00:57
|
|
CSM/LM undocked
|
|
May 22, 1969
|
23:34:16
|
|
LM ascent stage and descent stage separated
|
|
May 23, 1969
|
03:11:02
|
|
LM docked with CSM
|
|
May 23, 1969
|
05:13:36
|
|
LM ascent stage jettisoned
|
|
May 24, 1969
|
10:25:28
|
|
Transearth injection ignition (SPS)
|
|
May 24, 1969
|
10:28:13
|
|
Engine cutoff
|
|
May 26, 1969
|
16:22:26
|
|
Command and Service Modules (CM/SM) separation
|
|
May 26, 1969
|
16:37:54
|
|
Entry
|
|
May 26, 1969
|
16:52:23
|
|
Splashdown of spacecraft
"Apollo-10"
(crew:
Stafford,
Young,
Cernan
).
|